N1545X

Part: WIRE HARNESS — BROKEN (MLG DOOR) · airframe 24,466 hrs

GEAR DOOR EXPLOSIVE LINK CABLE ASSEMBLY BROKEN. SCRAPPED.

Part: GPS — WILL NOT TEST (COCKPIT) · airframe 24,461 hrs

2 YEAR INSPECTION. INSPECTED AND FOUND UNIT WOULD NOT PASS GPS TEST. RESET MEMORY AND RETESTED. NO HELP.

Part: FUEL CONTROL — MALFUNCTIONED (ENGINE) · airframe 24,457 hrs

FUEL CONTROL PRODUCING TORQUE SPLITS. TO BE SENT TO VENDOR.

Part: IGNITER — CRACKED (ENGINE) · airframe 24,454 hrs

IGNITER INSULATOR CRACKED. TO BE SENT TO VENDOR FOR REPAIR.

Part: ACTUATOR — STICKING (AFCS)

AFCS ACTUATOR STICKING. REPAIRED.

Part: ACTUATOR — MALFUNCTIONED (AFCS)

AFCS ACTUATOR KICKING. REPAIRED.

Part: BEARING — WORN (ROTATING SCISSOR)

ROTATING SCISSOR HAS WORN BEARINGS. REPLACED 4 EACH BEARINGS SB5200103 DUE TO BEING WORN. REPAIRED.

Part: BLADE — CORRODED (MAIN ROTOR) · airframe 24,195 hrs

THE C BLOCK HAS EXCESSIVE CORROSION AROUND THE ATTACHMENT BOLT. THE SKIN ON THE LOWER SIDE NEAR STA. 44 HAS SOME SEPERATION OVER THE SPAR. SENT TO INTERNATIONAL AVIATION COMPOSITES FOR INSPECTION AND REPAIR.

Part: BRUSHES — WORN (STARTER GEN)

STARTER GENERATOR MOTORING. REPLACED 4 BRUSHES DUE TO WORN. REPAIRED.

Part: MIXER BOX — MALFUNCTIONED (COCKPIT) · airframe 23,899 hrs

VHF SWITCHES WILL NOT MUTE AUDIO. FOUND SWITCH S1 BAD. REPLACED. BENCH CHECK GOOD.

Part: STARTER GEN — INOPERATIVE (ENGINE)

STARTER GEN INOPERATIVE.

Part: GYRO — FAILED (COCKPIT) · airframe 23,521 hrs

VERTICAL GYRO SPINS IN PITCH AND ROLL, OFF FLAG WILL NOT PULL.

Part: ANTENNA — DAMAGED (WX RADAR SYS) · airframe 23,422 hrs

NO SIGNAL ON INDICATOR. ANTENNA MALFUNCTION. SCRAPPED.

Part: INTERPHONE — DAMAGED (CABIN) · airframe 23,478 hrs

CANNOT EQUALIZE VOL BETWEEN VHF AND INT. COULD NOT VERIFY COMPLAINT. TOUCHED UP PAINT. BENCH CHECK GOOD.

Part: RELAY — FAILED (DC GENERATOR) · airframe 23,520 hrs

NR 2 GENERATOR REQUIRES RESET AFTER EACH START.

Part: ACTUATOR — INOPERATIVE (AFCS) · airframe 23,478 hrs

AFCS ACTUATOR INOPERATIVE.

Part: LINE — CHAFED (EMERGENCY FLOAT) · airframe 23,569 hrs

RT EMERGENCY FLOAT FLOAT LINE FROM BAG TO MANIFOLD CHAFED. SCRAPPED.

Part: AMPLIFIER — MALFUNCTIONED (VIB ABSORBER) · airframe 23,521 hrs

VTA WILL NOT TUNE.

Part: RADAR — MALFUNCTIONED (WX SYSTEM) · airframe 23,468 hrs

ERROR CODE 30 AND RECONFIGURING DOES NOT HELP. REPAIRED.

Part: DISPLAY — INOPERATIVE (WX RADAR SYS) · airframe 23,422 hrs

WEATHER RADAR DISPLAY HAS AN INOPERATIVE DISPLAY.

Part: BEARING — WORN (MAIN ROTOR) · airframe 23,425 hrs

MAIN ROTOR HAS A WORN BEARING. SCRAPPED.

Part: VTA ACTUATOR — LEAKING (M/R SYSTEM) · airframe 23,454 hrs

VTA ACTUATOR LEAKING.

Part: ANTENNA — BROKEN (WX RADAR SYS) · airframe 23,483 hrs

WEATHER RADAR OFF FLAG FLICKERS. FOUND ANTENNA TO BE BROKEN BEYOND REPAIR. SCRAPPED.

Part: BEARING — WORN (BELLCRANK) · airframe 23,468 hrs

WORN BEARINGS. REPAIRED.

Part: SCREEN — CRACKED (INTAKE) · airframe 23,402 hrs

RT INTAKE SCREEN CRACKED. SCRAPPED.

Part: DISPLAY — INOPERATIVE (WX RADAR SYS) · airframe 23,433 hrs

WEATHER RADAR SYSTEM DISPLAY INOPERATIVE.

Part: INDICATOR — BURNED OUT (WX RADAR SYS) · airframe 23,433 hrs

WEATHER RADAR SYSTEM CAUSED TWO INDICATORS TO BURN OUT. REPAIRED.

Part: ELBOW — DETERIORATED (EMERGENCY FLOAT) · airframe 23,571 hrs

ELBOW ON EMERGENCY FLOAT IS DETERIORATED.

Part: GENERATOR — INOPERATIVE (AC SYSTEM) · airframe 23,592 hrs

GENERATOR INOPERATIVE AFTER FLYING THROUGH HEAVY RAIN.

Part: CHECK VALVE — MALFUNCTIONED (FUEL SYS) · airframe 23,561 hrs

FUEL CHECK VALVE HARD TO START ON FIRST START. SCRAPPED.

Part: FLOAT — LEAKING (MLG) · airframe 23,569 hrs

RT MAIN LANDING GEAR EMERGENCY FLOAT BAG LEAKING.

Part: GCU — INOPERATIVE (AC SYSTEM) · airframe 23,589 hrs

AC GENERATOR GCU INOPERATIVE.

Part: GCU — WILL NOT TEST (AC SYSTEM) · airframe 23,443 hrs

AC GENERATOR CONTROL UNIT WOULD NOT TEST IN OVERVOLTAGE CHECK.

Part: PRESSURE SWITCH — MALFUNCTIONED (HEATER) · airframe 23,396 hrs

HEATER SWITCH ON TRANSMISSION LIGHT WOULD NOT COME ON. SCRAPPED.

Part: GYRO — MELTED (COCKPIT) · airframe 23,483 hrs

VERTICAL GYRO CAUSES KICK IN AFCS.

Part: RELAY — INOPERATIVE (DC SYSTEM) · airframe 23,389 hrs

BUS TIE RELAY CONTACTOR INOPERATIVE.

Part: INDICATOR — RATCHETING (COCKPIT) · airframe 23,483 hrs

ATTITUDE INDICATOR HAS RATCHETY MOVEMENT.

Part: SKIN — ERODED (M/R BLADE) · airframe 23,438 hrs

MAIN ROTOR BLADE FIBERGLASS SKIN NEAR THE OUTBOARD END IS ERODED BEYOND LIMITS.

Part: INDICATOR — MALFUNCTIONED (WX RADAR SYS) · airframe 23,726 hrs

INDICATOR SPIKING. PENDING VENDOR REPAIR.

Part: AMPLIFIER — FAILED (FIRE WARNING) · airframe 23,521 hrs

FIRE WARNING WILL NOT TEST. REPLACE THE CONTROL AMPLIFIER.

Part: AMPLIFIER — FAILED (AFCS) · airframe 23,501 hrs

AFCS ROLL SLICE (ROLL CHANNEL KICKS IN FLIGHT).

Part: TRANSCEIVER — INTERMITTENT (COCKPIT) · airframe 23,569 hrs

TRANSCEIVER INTERMITTENTLY INOPERATIVE.

Part: TIP CAP — DAMAGED (M/R BLADE)

MAIN ROTOR BLADE TIP CAP HAS FIBERGLASS BETWEEN INTERNAL AND EXTERNAL DOUBLER BROKEN. CRACK IN THE ABRASION STRIP ON THE LOWER SIDE.

Part: INDICATOR — MALFUNCTIONED (RADAR ALTIMETER) · airframe 23,392 hrs

RADAR ALTIMETER INDICATOR HAS AN UNRELIABLE OFF FLAG AND NEEDLE PARKS DURING FLIGHT.

Part: TACHOMETER — MALFUNCTIONED (COCKPIT) · airframe 23,569 hrs

TACHOMETER MALFUNCTIONED, OVERSPEED LIGHT STAYS ON.

Part: SCREW — CORRODED (LUBE PUMP ADJUST)

MAIN ROTOR GEARBOX LUBE OIL PUMP ADJUSTMENT SCREW CORRODED.

Part: BLADE — DAMAGED (MAIN ROTOR) · airframe 23,289 hrs

MAIN ROTOR BLADE FIBERGLASS BEHIND THE SPLICE AREA IS TORN AND SEPARATED BEYOND LIMITS. HELICOIL AT THE ROOT END IS STRIPPED.

Part: ROD END — CRACKED (MLG) · airframe 21,314 hrs

BEARING IS CRACKED END TO END ON ONE SIDE. SCRAPPED.

Part: MIXER BOX — MALFUNCTIONED (CABIN) · airframe 23,298 hrs

BLEED OVER TO OTHER CHANNELS OF MIXER BOX WITHOUT SWITCH SELECTED. PERFORMED PRELIMINARY INSPECTION. FOUND SWITCH S1 AND SELECTOR KNOB BAD. REPLACED AND REPAIRED. BENCH CHECK GOOD.

Part: GEARSHAFT — SPALLED (GEARBOX) · airframe 23,285 hrs

GEARSHAFT IN GEARBOX HAS SPALLING ON GEARTEETH.

Part: BEARING — SPALLED (GEARBOX) · airframe 23,285 hrs

GEAR HAS SPALLING ON BALL BEARING.

Part: BLADE — DAMAGED (TAIL ROTOR) · airframe 22,637 hrs

TRAILING EDGE OF PADDLE A IS SPLIT OPEN. THE CENTER PLUG IS ALSO DEBONDED. SENT TO INTERNATIONAL AVIATION COMPOSITES FOR INSPECTION AND REPAIR.

Part: ALTIMETER — FAILED (COCKPIT)

ALTIMETER READ 75-100 ON GROUND 100-150 AT ALTITUDE.

Part: GCU — FAILED (AC SYSTEM)

UNDERVOLT WILL NOT TEST.

Part: GEAR — SPALLED (GEARBOX)

ENGINE REMOVED DUE TO METAL IN OIL. UPON INSPECTION OF GEARBOX PARTS NOTED: SPALLING OF GEAR TEETH. INSTALLED NEW PARTS.

Part: PINION GEAR — SPALLED (GEARBOX)

ENGINE REMOVED DUE TO METAL IN OIL. UPON INSPECTION OF GEARBOX PARTS NOTED: SPALLING OF GEAR TEETH. INSTALLED NEW PARTS.

Part: NOZZLE — CRACKED (1ST STAGE)

ENGINE REMOVED DUE TO TURBINE OVERHAUL. UPON INSPECTION OF TURBINE PARTS NOTED CRACKS BEYOND SERVICEABLE LIMITS ON 1ST STAGE NOZZLE VANES.

Part: INDICATOR — MALFUNCTIONED (ADI)

TURN INDICATOR OFF TO RIGHT.

Part: DIFFUSER — LEAKING (NR 2 BEARING)

ENGINE REMOVED DUE TO METAL IN OIL. FOUND REAR SUPPORT MAJOR SEAL LIFTING AND CHROME FITTING FLAKING IN NR 2 BEARING BORE. REPLACED WITH SERVICEABLE REAR DIFFUSER.

Part: PINION GEAR — WORN (GEARBOX)

ENGINE REMOVED DUE TO METAL IN OIL. FOUND CAUSE: PICKOUT IN GEAR TEETH. REPLACED WITH SERVICEABLE GEAR. SCRAPPED GEAR.

Part: CARBON SEAL — LEAKING (NR 1 BEARING)

ENGINE REMOVED DUE TO NR 1 SEAL LEAK. UPON INSPECTION, FOUND SLOT WEAR IN CARBON SEAL RING. PART SCRAPPED.

Part: TIP CAP — ERODED (M/R BLADE)

END CAP IS ERRODED THROUGH.

Part: GYRO — INOPERATIVE (COCKPIT)

VERTICAL GYRO INOPERATIVE. WILL NOT COME UP TO SPEED.

Part: ACTUATOR — LEAKING (MAIN ROTOR)

ACTUATOR LEAKING.

Part: BLADE — BULGING (MAIN ROTOR)

LEADING EDGE BULGING OUTWARD.

Part: TRANSCEIVER — MALFUNCTIONED (COCKPIT)

TRANSCEIVER HAS WEAK AND SCRATCHY OPERATION.

Part: SEAL — PITTED (ENGINE)

ENGINE REMOVED DUE TO METAL. UPON INSPECTION OF COMPRESSOR PARTS NOTED: PITS BEYOND SERVICEABLE LIMITS ON SEAL CARBON FACE. INSTALLED A NEW SEAL.

Part: GPS — INOPERATIVE (COCKPIT)

GPS INOPERATIVE.

Part: RATE GYRO — MALFUNCTIONED (COCKPIT)

GP RATE OF TURN, GYRO FLAG DOES NOT PULL.

Part: DAMPER — LEAKING (MAIN ROTOR)

MAIN ROTOR DAMPER IS WEAK AND LEAKS.

Part: DAMPER — LEAKING (MAIN ROTOR)

MAIN ROTOR DAMPER IS WEAK AND LEAKS.

Part: TRANSCEIVER — MALFUNCTIONED (COCKPIT)

TRANSMIT SIDETONE GARBLED. TESTED, CLEANED CORROSION, BENCH CHECK GOOD.

Part: FLOAT BAG — LEAKING (FLOAT)

FLOAT BAG LEAKING.

Part: PUMP — LEAKING (HYDRAULIC SYS)

HYDRAULIC PUMP LEAKS FROM SEAL DRAIN.

Part: CAUTION PANEL — MALFUNCTIONED (COCKPIT)

BATTERY TEMP WARNING LIGHT INOPERATIVE.

Part: SPUR GEAR — WORN (ENGINE)

ENGINE REMOVED DUE TO IMPELLER TIME. INSPECTION OF COMPRESSOR PARTS NOTED: STEP WEAR BEYOND SERVICEABLE LIMITS ON SHAFT SPLINES.

Part: BLADE — DAMAGED (TAIL ROTOR)

PADDLE 'A' HAS A HOLE IN THE LEADING EDGE ABRASION STRIP.

Part: ACUTATOR — MALFUNCTIONED (ENGINE CONTROL)

ACTUATOR MOTOR STICKS INTERMITTENTLY.

Part: RECEIVER — INOPERATIVE (COCKPIT GPS)

TO/FROM POINTER INOPERATIVE ON NAVIGATOR INDICATOR.

Part: CONTROL UNIT — FAILED (DC SYSTEM)

GENERATOR WILL NOT RESET WHEN TESTING FOR GROUND FAULT OR OVER VOLTAGE.

Part: SUPPORT — DEFECTIVE (GP SECTION)

RECEIVING INSPECTION REVEALED: EXCESSIVE RUNOUT .013 INCH BEYOND SERVICEABLE LIMITS ON G.P. SUPPORT FORWARD FLANGE. INSTALLED A DALLAS AIRMOTIVE OVERHAULED G.P. SUPPORT.

Part: COLLECTOR RING — DEFECTIVE (TURBINE SECTION)

RECEIVING INSPECTION REVEALED: EXCESSIVE RUNOUT .010 INCH BEYOND SERVICEABLE LIMITS ON EXHAUST COLLECTOR. FORWARD PILOT AND VENT ORIFICE TUBE OUT OF ROUND. INSTALLED A DALLAS AIRMOTIVE OVERHAULED EXHAUST COLLECTOR.

Part: INDICATOR — READS LOW (ENGINE OIL)

OIL TEMPERATURE SIDE READS LOW.

Part: ACTUATOR — MALFUNCTIONED (ENGINE CONTROL)

MOTOR ROTATES TOO LONG BEFORE SHAFT MOVES.

Part: ACTUATOR — MALFUNCTIONED (ENGINE CONTROL)

ACTUATOR MOTOR ROUTES TOO LONG BEFORE SHAFT TURNS.

Part: INDICATOR — FAILED (FUEL QUANTITY)

NR 2 FLUCTUATES AND WILL NOT CALIBRATE.

Part: GENERATOR — WORN (AC SYS)

A/C GEN WORN AND DRY DRIVESHAFT AND ROTOR SPLINES.

Part: INDICATOR — FLUCTUATES (ENG OIL)

NEEDLE FLUCTUATES AT 50' INTERMITTENTLY.

Part: DETECTOR — INTERMITTENT (SMOKE DET)

SMOKE DET INTERMITTENT WARNING LIGHTS.

Part: SMOKE DETECTOR — FAILED (FIRE SYS)

SMOKE DETECTOR WILL NOT TEST.

Part: TIP CAP — DEFECTIVE (M/R)

BOTH INTERNAL DOUBLERS HAVE RIVETS INSTALLED.

Part: DAMPER — LEAKING (M/R)

VISCIOUS DAMPER LEAKING AND WEAK.

Part: FUEL PUMP — WORN (ENG FUEL)

FUEL PUMP WORN SPLINES.

Part: BLADE — SEPARATION (M/R)

FIBERGLASS SEPARATED UNDERNEATH THE SLICE TITANIUM AT STATION 112.5 ON BOTH SURFACES. THE TRIM TAB HAS SOME SEPARATION ALSO.

Part: DC CONTROL UNIT — FAILED (DC SYS)

GENERATOR WOULD NOT COME ON LINE.

Part: INVERTER — FAILED (AC SYS)

INVERTER CYCLES ON AND OFF.

Part: GENERATOR — FAILED (AC SYS)

AC GENERATOR INOPERATIVE. THIS IS THE THIRD TIME THIS GENERATOR WAS REMOVED FOR BEING INOPERATIVE SINCE WE RECEIVED IT OVERHAULED 2-28-97.

Part: GENERATOR — FAILED (AC SYS)

A/C WILL NOT COME ON LINE DUE TO GENERATOR FAILED.

Part: BLADE — SEPARATION (M/R)

M/R BLADE FIBERGLASS SEPARATED UNDERNEATH THE SPLICE TITANIUM AT STATION 112.5 ON BOTH SURFACES. THE TRIM TAB HAS SOME SEPARATION ALSO.

Part: DAMPER — WORN (M/R)

M/R DAMPER WEAR SPOT ON PISTON.

Part: INVERTER — FAILED (AC SYS)

INVERTER CYCLES ON AND OFF.

Part: BEARING — SEPARATED (M/R DRIVE)

BEARING SEPARATION BEYOND LIMITS.

Part: EJECTOR — CRACKED (EXHAUST)

EJECTOR HAS EXCESSIVE CRACKING.

Part: BEARING — SEPARATED (SPINDLE ASSY)

BEARING SEPARATED BEYOND LIMITS.

Part: SWITCH — FAILED (OIL PRESS)

CAUTION LIGHT STAYS ON WITH OIL PRESSURE.

Part: BLOWER — SMOKING (COCKPIT)

BLOWER EMITS A SMOKE ODOR.

Part: NOZZLE — EXCESS RUNOUT (ENG NR 2)

RECEIVING INSPECTION REVEALED: EXCESSIVE RUNOUT (.010) OF #2 NOZZLE 29-34 SEAL BORE. INSTALLED A NEW #2 NOZZLE.

Part: ALTIMETER — ERROR (COCKPIT)

ALTIMETER INACCURATE READING OVER 125 FEET OFF.

Part: ALTIMETER — ERROR (COCKPIT)

ALTIMETER HAS INACCURATE READING OVER 125.

Part: REAR DIFFUSER — DEFECTIVE (ENGINE)

ASSEMBLY REQUIREMENT REVEALED: EXCESSIVE RUN OUT (.0045) OF REAR DIFFUSER #2 BEARING BORE (MAX RUN OUT .002) RE-INDEXED SHROUD NO CHANGE. #2 BEARING BORE .003 BELOW SPECS. INSTALLED A DALLAS AIRMOTIVE OVERHAULED REAR DIFFUSER.

Part: GENERATOR — WORN SHAFT (A/C SYS)

A/C GENERATOR WORN SHAFT AND ROTOR SPLINES.

Part: INDICATOR — STICKS (TURB TEMP)

POWER TURBINE TEMP STICKS ON 600 DEGREE C.

Part: GENERATOR — FAILED (AC SYS)

GENERATOR WILL NOT COME ON LINE.

Part: GYRO — MALFUNCTION (COCKPIT ATTITUDE)

ATTITUDE FLAG WILL NOT PULL.

Part: VERTICAL GYRO — PRECESSES (COCKPIT ADI)

ADI PRECESSES INTERMITTENTLY.

Part: INDICATOR — STUCK (RATE OF CLIMB)

RATE OF CLIMB NEEDLE SETTING AT 1500 FEET FPM DECENT STATIC.

Part: BLADE — DEFECTIVE (T/R TIP)

PADDLE "A" OF THE ASSEMBLY HAS A VOID OVER THE TIP WEIGHT COVER.

Part: TIP CAP — TORN (M/R BLADE)

TIP CAP HAS THE SKIN TORN ON THE LOWER SIDE BEYOND THE MAXIMUM LIMITS.

Part: TIP CAP — HOLED (M/R BLADE LE)

TIP CAP HAS A HOLE IN THE LOWER SKIN JUST AFT OF THE LEADING EDGE ABRASION STRIP.

Part: REPEATER — FAILED (ENG OIL)

REPEATER ALL LED'S DO NOT WORK PROPERLY.

Part: ACUTATOR — FAILED (ENGINE)

ACTUATOR MOTOR TURNS -- SHAFT WILL NOT TURN.

Part: TIP CAP — DAMAGED (M/R)

TIP CAP HAS EXCESSIVE DAMAGE ON THE TRAILING EDGE NEAR THE INBOARD END.

Part: CVR — WONT TEST (COCKPIT)

CVR WILL NOT TEST PROPERLY.

Part: BLADE — SEPARATION (TIP RIB)

SEPARATION IN THE SKIN NEAR THE TIP RIB AREA WITH CRACKS IN THE SKIN JUST BELOW THE SPAR ON THE LOWER SIDE.

Part: TIP CAP — CRACKED (MR BLADE)

TIP CAP HAS ABRASION STRIP CRACKED WITH SEPARATION. FIBERGLASS BROKEN BETWEEN THE DOUBLER ON THE UPPER SURFACE.

Part: CABLE ASSEMBLY — MIS MFG (T/R CONTROL)

CABLE 1/2 INCH TOO SHORT WHEN MEASURED AGAINST OLD T/R CABLE. WHEN INSTALLED IN AIRCRAFT EXPOSED THREAD ON TURNBUCKLE OUT OF LIMITS WITH CORRECT CABLE TENSION.

Part: SERVO — WORN (M/R)

INPUT LEVER BEARINGS WORN. SENT TO HASE FOR MODIFICATION FOR CSN76-173 AND HR TEXTRON S.B. 0006760-06.

Part: TIP CAP — CRACKED (M/R BLADE)

TIP CAP HAS THE ABRASION STRIP CRACKED WITH MULTIPLE BRANCHES AND SEPARATION. ALSO HAS SOME FIBERGLASS EROSION.

Part: INDICATOR — FAILED (COCKPIT)

UNIT HAS A BAD TEST PATTERN AND ALL GREEN DISPLAY.

Part: TRANSCEIVER — INOPERATIVE (COCKPIT)

TRANSCEIVER INOPERATIVE AFTER WARM UP. TIME SINCE REPAIR 0:00.

Part: ANTENNA — WEAK (LORAN)

LORAN ANTENNA WEAK SIGNAL STRENGTH.

Part: INDICICATOR — INOPERATIVE (ENG OIL)

ENGINE TEMP INDICATOR INOPERATIVE.

Part: BRACKET — BROKE (M/R HUB WEIGHT)

DURING THE PROCESS OF LOOSENING M/R WEIGHT BOLT FOR ROUTINE M/R TRACK AND BALANCE, HUB BALANCE BRACKET BROKE IN TWO PIECES. BREAK WAS IN AREA OF 90 DEGREE BEND APPROX. 10% OF FRACTURE AREA APPEARS TO BE A FRESH BREAK. INSPECTED M/R WEIGHT STICK-UPAND FOUND TO BE INSTALLED PROPERLY.

Part: VERTICAL GYRO — DEFECTIVE (AFCS PITCH)

KICK IN AFCS PITCH CHANNEL.

Part: ALTIMETER — ERROR (COCKPIT)

ALTIMETER NEEDLE INDICATES 120 FEET OFF AT ZERO.

Part: ANTENNA — DEFECTIVE (LORAN)

WILL NOT LOCK ON TO SIGNAL.

Part: INDICATOR — FAULTY (COCKPIT)

INDICATOR DROPS OFF LINE AND HAS INTERMITTENT GLICK ON SCREEN.

Part: R/T UNIT — DEFECTIVE (RADAR)

R/T UNIT HAS BAD IF BOARD AND BAD MODULATOR BOARD CAUSING UNIT TO DROP OFF LINE IN MAP MODE. ALSO GAIN VOLTAGE IS OUT OF SPECS. AT MAXIMUM GAIN, UNABLE TO ADJUST.

Part: CONTROL UNIT — DEFECTIVE (DC SYS)

CONTROL UNIT DEFECTIVE. #2 D.C. GENERATOR WOULD NOT COME ON LINE.

Part: BLADE — SPLIT (T/R)

PADDLE "A" SPLIT OPEN ON THE TRAILING EDGE AT THE ATTACHMENT AREA.

Part: GYRO — DEFECTIVE (COCKPIT VG)

VERT GYRO KEEPS IN ROLL.

Part: GYRO — DEFECTIVE (COCKPIT VG)

VERT GYRO KEEPS IN ROLL.

Part: INDICATOR — DEFECTIVE (COCKPIT)

TEST PATTERN SPOKES INTERMITTENTLY.

Part: TRANSCEIVER — DEFECTIVE (COCKPIT VHF)

UNIT STARTS TRANSMITTING AS SOON AS POWER IS APPLIED. SENT TO THE RADIO SHOP FOR INSPECTION AND REPAIR.

Part: WINDOW — CRACKED (RT AIRFRAME)

THE R/H WINDOW WHEN INSTALLED, CRACKED IN THE UPPER R/H CORNER. LOWER CORNER OF THE WINDOW EXTENDS 3 1/2" WHEN LAYED ON THE AIRFRAME. THIS DISTANCE CREATES EXCESSIVE STRESS DURING INSTALLATION.

Part: WINDOW — DEFECTIVE (PILOT DOOR)

OPENABLE WINDOW NOT CUT OUT.

Part: EJECTOR — CRACKED (EXHAUST)

EJECTORS CRACKED IN SEVERAL PLACES.

Part: ALTIMETER — CASE LEAK (COCKPIT)

UNIT HAS EXCESSIVE CASE LEAK.

Part: GYRO — DEFECTIVE (COCKPIT VG)

SLOW TO SCROLL AFTER START UP.

Part: BLADE — CRACKED (T/R)

CRACK ON THE ABRASION STRIP WITH MULTIPLE BRANCH ON PADDLE "B".

Part: ACTUATOR — DEFECTIVE (AFCS)

ACTUATOR CHATTERS.

Part: ACTUATOR — CHATTERING (AFCS)

ACTUATOR CHATTERING.

Part: BLADE — CRACKED (M/R)

NUMEROUS CRACKS ON THE NICKEL STRIP. THE TIP RIB IS PARTIALLY UNBONDED. THERE ARE NO MODIFICATIONS DONE TO THE TIP END FOR THE CSN TO BE COMPLIED WITH AND THIS BLADE ALSO MEETS THE TIME REQUIREMENT FOR THE ULTRA SONIC INSPECTION FOR TIME EXTENSION.

Part: TRANSCEIVER — CORRODED (COCKPIT)

BENCH CHECK REQUIRED. INSPECTED AND FOUND CORROSION. CLEANED CORROSION ON CHASIS AND APPLIED ALODINE. FOUND C101 CAPACITOR ON POWER SUPPLY BOARD HAD LEAKAGE. REPLACED C101 CAPACITOR. REPAIRED. BENCH CHECK GOOD.

Part: CVR — WONT TEST (COCKPIT)

WILL NOT TEST AUDIO-NO 400 HZ TONE. FIVE YEAR INSPECTION DUE 8/96.